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36NiCrMo16 / 1.6773 is a high-strength alloy steel belonging to the European standard EN 10083-3 and EN 10250-3. It is widely used in demanding industries such as aerospace, automotive engineering, heavy machinery, and high-performance components due to its exceptional mechanical properties.
36NiCrMo16 is a Ni-Cr-Mo alloy steel with a carbon content of 0.32-0.39%, offering excellent hardenability, toughness, and fatigue resistance. After quenching and tempering, it achieves a superior combination of high tensile strength, impact resistance, and wear durability, making it ideal for critical structural components, gears, shafts, and high-stress applications.
1: Steel equivalent
Country | Europe |
Standard | EN10083-3 |
Grade | 36NiCrMo16/1.6773 |
2: Chemical composition
Grade | C | Si | Mn | P | S | Cr | Mo | Ni |
36NiCrMo16/1.6773 | 0.32-0.39 | 0.4Max | 0.5-0.8 | 0.025Max | 0.025Max | 1.6-2.0 | 0.25-0.45 | 3.6-4.1 |
3: Mechanical properties .
Mechanical properties for 36NiCrMo16 quenching and tempering alloy steel according to EN10083-3.
Size range | Tensile strength | Yield strength | Alongation | Area of reduction | Impact value At RT/J |
d≤16 t≤8 | 1250-1450Mpa | 1050Mpa Min | 9% Min | 40% Min | / |
16<d≤40 8<t≤20 | 1250-1450Mpa | 1050Mpa Min | 9% Min | 40%Min | 30J Min |
40<d≤100 20<t≤60 | 1100-1300Mpa | 900Mpa Min | 10% Min | 45%Min | 35J Min |
100<d≤160 60<t≤100 | 1000-1200Mpa | 800Mpa Min | 11% Min | 50%Min | 45J Min |
160<d≤250 100<t≤160 | 1000-1200Mpa | 800Mpa Min | 11% Min | 50%Min | 45J Min |
Sampling and preparation of test pieces for 36NiCrMo16 quenching and tempering steel.
1): According to EN10083-1, all samples shall be taken at a distance of 12.5mm below the heat treated surface
2): As stipulated in the contract between buyer and seller.
Mechanical properties for 36NiCrMo16 open die forgings steel according to EN10250-3
Size range | Tensile strength | Yield strength | Alongation | Impact value at RT/J | ||
L | Tr | L | Tr | |||
d≤160 | 1000Mpa Min | 800Mpa Min | 11% Min | 8% Min | 45J Min | 22J Min |
160<d≤330 | 1000Mpa Min | 800Mpa Min | 11% Min | 8% Min | 45J Min | 22J Min |
330<d≤660 | 1000Mpa Min | 800Mpa Min | 11% Min | 8% Min | 45J Min | 22J Min |
Remark: L= Longitudinal Tr = Transverse
Sampling and preparation of test pieces for steel forging.
1: According to EN10250-1, all samples shall be taken at a distance of 4/T below the heat treated surface (with a minimum of 20mm and a maximum of 80mm), and t/2 from the end (where t is the equivalent thickness of the thickness of the ruling section of the forging at the time of heat treatment.
2: As stipulated in the contract between buyer and seller.
4: Surface hardness and hardenability.
Heat Treatment | Hardness |
Flame or Induction hardening | 53HRC |
Soft annealed (+A) | HB269Max |
Quenched and tempred (+QT) | HRC28-32(Common Range) |
Where the steel is ordered by using the symbols for normal (+H) or restricted (+HL, +HH) hardenability requirements, the hardenability values should apply below:
Distance in mm from quenched end | ||||||||||||||||
Distance | 1.5 | 3 | 5 | 7 | 9 | 11 | 13 | 15 | 20 | 25 | 30 | 35 | 40 | 45 | 50 | |
Hardness In HRC + H | max | 57 | 56 | 56 | 56 | 56 | 56 | 55 | 55 | 55 | 55 | 55 | 55 | 55 | 55 | 55 |
min | 50 | 49 | 48 | 48 | 48 | 48 | 47 | 47 | 47 | 47 | 47 | 47 | 47 | 47 | 47 | |
Hardness In HRC + HH | max | 57 | 56 | 56 | 56 | 56 | 56 | 55 | 55 | 55 | 55 | 55 | 55 | 55 | 55 | 55 |
min | 52 | 51 | 51 | 51 | 51 | 51 | 50 | 50 | 50 | 50 | 50 | 50 | 50 | 50 | 50 | |
Hardness In HRC + HL | max | 55 | 54 | 53 | 53 | 53 | 53 | 52 | 52 | 52 | 52 | 52 | 52 | 52 | 52 | 52 |
min | 50 | 49 | 48 | 48 | 48 | 48 | 47 | 47 | 47 | 47 | 47 | 47 | 47 | 47 | 47 |
Scatter bands for the Rockwell - C hardness in the end quench hardenability test.
5: Supply size & Tolerance & Stock size
Product type | Size range | Length |
Cold drawn bar | Φ3-Φ80mm | 6000-9000mm |
Hot rolled bar | Φ16-Φ310mm | 6000-9000mm |
Hot forged bar | Φ100-Φ1200mm | 3000-5800mm |
Hot rolled plate/sheet | T:3-200mm; W:1500-2500mm | 2000-5800mm |
Hot Forged block | T: 80-800mm; W: 100-2500mm | 2000-5800mm |
Surface Finish | Turned | Milled | Grinding(Best) | Polished(Best) | Peeled(Best) | Black Forged | Black Rolled |
Tolerance | +0/+3mm | +0/+3mm | +0/+0.05mm | +0/+0.05mm | +0/+0.1mm | +0/+5mm | +0/+1mm |
Straighness | 1mm/1000mm max. | 3mm/1000mm max. |
For this material, there is no stocks for both hot rolled bar and hot forged bar, because China domestic used it very rarely, so no stockiest will stock them. If we want to order 36NiCrMo16 material, usually the MOQ is 10tons.
6:Forging processing
Put the 36NiCrMo16 ingot into the furnace and heat to 1150-1200℃
Forge the ingot, forging temperature should be not less than 850-900℃
Cooling in the air or in the furnace after forged
7: Heat treatment
Soft annealed:
Heat 36NiCrMo16 steel to 650-700℃ in the furnace
Soak at this temperature in the furnace
Cooling in the furnace
Normalized:
Heat 36NiCrMo16 steel to 880-950℃ in the furnace
Soak at this temperature in the furnace
Cooling in the air
Quenching and tempering:
Heat 36NiCrMo16 steel to 865-885℃ in the furnace
Soak at this temperature in the furnace
Quench in water, oil or air
Temper steel at 550-650℃ in the furnace
Take out of 36NiCrMo16 steel from furnace and cool in the air.
Remark: The conditions given above are for guidance, at the temperatures at the lower end of the range are generally applicable to hardening in water and those at the upper end for hardening in oil.
8: Weldability
36NiCrMo16 steel has relatively poor weldability. For steel materials, weldability is strongly related to the carbon content. When the carbon content exceeds 0.25%, weldability begins to deteriorate. The carbon content of 36NiCrMo16 is approximately 0.36%, so its weldability is not ideal. Additionally, the high nickel and chromium content in this alloy steel can further increase the risk of cracking during welding.
9:Application
36NiCrMo16 is a high-strength, high-toughness alloy structural steel, which is widely used in key components requiring high mechanical properties and fatigue strength. Its main application areas include:
1): Used in the manufacture of aircraft landing gear, engine drive shafts, turbine components and other key load-bearing parts.
2): Used in the manufacture of high performance engine crankshafts, connecting rods, transmission gears and other key moving parts.
3): Used in the manufacture of crankshafts for large diesel engines, gas turbine shafts, gears and bearing parts for mining machinery.
4): Suitable for manufacturing high load gears, bearings, precision shaft parts, etc.
36NiCrMo16 / 1.6773 is a high-strength alloy steel belonging to the European standard EN 10083-3 and EN 10250-3. It is widely used in demanding industries such as aerospace, automotive engineering, heavy machinery, and high-performance components due to its exceptional mechanical properties.
36NiCrMo16 is a Ni-Cr-Mo alloy steel with a carbon content of 0.32-0.39%, offering excellent hardenability, toughness, and fatigue resistance. After quenching and tempering, it achieves a superior combination of high tensile strength, impact resistance, and wear durability, making it ideal for critical structural components, gears, shafts, and high-stress applications.
1: Steel equivalent
Country | Europe |
Standard | EN10083-3 |
Grade | 36NiCrMo16/1.6773 |
2: Chemical composition
Grade | C | Si | Mn | P | S | Cr | Mo | Ni |
36NiCrMo16/1.6773 | 0.32-0.39 | 0.4Max | 0.5-0.8 | 0.025Max | 0.025Max | 1.6-2.0 | 0.25-0.45 | 3.6-4.1 |
3: Mechanical properties .
Mechanical properties for 36NiCrMo16 quenching and tempering alloy steel according to EN10083-3.
Size range | Tensile strength | Yield strength | Alongation | Area of reduction | Impact value At RT/J |
d≤16 t≤8 | 1250-1450Mpa | 1050Mpa Min | 9% Min | 40% Min | / |
16<d≤40 8<t≤20 | 1250-1450Mpa | 1050Mpa Min | 9% Min | 40%Min | 30J Min |
40<d≤100 20<t≤60 | 1100-1300Mpa | 900Mpa Min | 10% Min | 45%Min | 35J Min |
100<d≤160 60<t≤100 | 1000-1200Mpa | 800Mpa Min | 11% Min | 50%Min | 45J Min |
160<d≤250 100<t≤160 | 1000-1200Mpa | 800Mpa Min | 11% Min | 50%Min | 45J Min |
Sampling and preparation of test pieces for 36NiCrMo16 quenching and tempering steel.
1): According to EN10083-1, all samples shall be taken at a distance of 12.5mm below the heat treated surface
2): As stipulated in the contract between buyer and seller.
Mechanical properties for 36NiCrMo16 open die forgings steel according to EN10250-3
Size range | Tensile strength | Yield strength | Alongation | Impact value at RT/J | ||
L | Tr | L | Tr | |||
d≤160 | 1000Mpa Min | 800Mpa Min | 11% Min | 8% Min | 45J Min | 22J Min |
160<d≤330 | 1000Mpa Min | 800Mpa Min | 11% Min | 8% Min | 45J Min | 22J Min |
330<d≤660 | 1000Mpa Min | 800Mpa Min | 11% Min | 8% Min | 45J Min | 22J Min |
Remark: L= Longitudinal Tr = Transverse
Sampling and preparation of test pieces for steel forging.
1: According to EN10250-1, all samples shall be taken at a distance of 4/T below the heat treated surface (with a minimum of 20mm and a maximum of 80mm), and t/2 from the end (where t is the equivalent thickness of the thickness of the ruling section of the forging at the time of heat treatment.
2: As stipulated in the contract between buyer and seller.
4: Surface hardness and hardenability.
Heat Treatment | Hardness |
Flame or Induction hardening | 53HRC |
Soft annealed (+A) | HB269Max |
Quenched and tempred (+QT) | HRC28-32(Common Range) |
Where the steel is ordered by using the symbols for normal (+H) or restricted (+HL, +HH) hardenability requirements, the hardenability values should apply below:
Distance in mm from quenched end | ||||||||||||||||
Distance | 1.5 | 3 | 5 | 7 | 9 | 11 | 13 | 15 | 20 | 25 | 30 | 35 | 40 | 45 | 50 | |
Hardness In HRC + H | max | 57 | 56 | 56 | 56 | 56 | 56 | 55 | 55 | 55 | 55 | 55 | 55 | 55 | 55 | 55 |
min | 50 | 49 | 48 | 48 | 48 | 48 | 47 | 47 | 47 | 47 | 47 | 47 | 47 | 47 | 47 | |
Hardness In HRC + HH | max | 57 | 56 | 56 | 56 | 56 | 56 | 55 | 55 | 55 | 55 | 55 | 55 | 55 | 55 | 55 |
min | 52 | 51 | 51 | 51 | 51 | 51 | 50 | 50 | 50 | 50 | 50 | 50 | 50 | 50 | 50 | |
Hardness In HRC + HL | max | 55 | 54 | 53 | 53 | 53 | 53 | 52 | 52 | 52 | 52 | 52 | 52 | 52 | 52 | 52 |
min | 50 | 49 | 48 | 48 | 48 | 48 | 47 | 47 | 47 | 47 | 47 | 47 | 47 | 47 | 47 |
Scatter bands for the Rockwell - C hardness in the end quench hardenability test.
5: Supply size & Tolerance & Stock size
Product type | Size range | Length |
Cold drawn bar | Φ3-Φ80mm | 6000-9000mm |
Hot rolled bar | Φ16-Φ310mm | 6000-9000mm |
Hot forged bar | Φ100-Φ1200mm | 3000-5800mm |
Hot rolled plate/sheet | T:3-200mm; W:1500-2500mm | 2000-5800mm |
Hot Forged block | T: 80-800mm; W: 100-2500mm | 2000-5800mm |
Surface Finish | Turned | Milled | Grinding(Best) | Polished(Best) | Peeled(Best) | Black Forged | Black Rolled |
Tolerance | +0/+3mm | +0/+3mm | +0/+0.05mm | +0/+0.05mm | +0/+0.1mm | +0/+5mm | +0/+1mm |
Straighness | 1mm/1000mm max. | 3mm/1000mm max. |
For this material, there is no stocks for both hot rolled bar and hot forged bar, because China domestic used it very rarely, so no stockiest will stock them. If we want to order 36NiCrMo16 material, usually the MOQ is 10tons.
6:Forging processing
Put the 36NiCrMo16 ingot into the furnace and heat to 1150-1200℃
Forge the ingot, forging temperature should be not less than 850-900℃
Cooling in the air or in the furnace after forged
7: Heat treatment
Soft annealed:
Heat 36NiCrMo16 steel to 650-700℃ in the furnace
Soak at this temperature in the furnace
Cooling in the furnace
Normalized:
Heat 36NiCrMo16 steel to 880-950℃ in the furnace
Soak at this temperature in the furnace
Cooling in the air
Quenching and tempering:
Heat 36NiCrMo16 steel to 865-885℃ in the furnace
Soak at this temperature in the furnace
Quench in water, oil or air
Temper steel at 550-650℃ in the furnace
Take out of 36NiCrMo16 steel from furnace and cool in the air.
Remark: The conditions given above are for guidance, at the temperatures at the lower end of the range are generally applicable to hardening in water and those at the upper end for hardening in oil.
8: Weldability
36NiCrMo16 steel has relatively poor weldability. For steel materials, weldability is strongly related to the carbon content. When the carbon content exceeds 0.25%, weldability begins to deteriorate. The carbon content of 36NiCrMo16 is approximately 0.36%, so its weldability is not ideal. Additionally, the high nickel and chromium content in this alloy steel can further increase the risk of cracking during welding.
9:Application
36NiCrMo16 is a high-strength, high-toughness alloy structural steel, which is widely used in key components requiring high mechanical properties and fatigue strength. Its main application areas include:
1): Used in the manufacture of aircraft landing gear, engine drive shafts, turbine components and other key load-bearing parts.
2): Used in the manufacture of high performance engine crankshafts, connecting rods, transmission gears and other key moving parts.
3): Used in the manufacture of crankshafts for large diesel engines, gas turbine shafts, gears and bearing parts for mining machinery.
4): Suitable for manufacturing high load gears, bearings, precision shaft parts, etc.